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A360.0 Aluminum vs. S41425 Stainless Steel

A360.0 aluminum belongs to the aluminum alloys classification, while S41425 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is A360.0 aluminum and the bottom bar is S41425 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75
280
Elastic (Young's, Tensile) Modulus, GPa 72
200
Elongation at Break, % 1.6 to 5.0
17
Fatigue Strength, MPa 82 to 150
450
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
77
Shear Strength, MPa 180
570
Tensile Strength: Ultimate (UTS), MPa 180 to 320
920
Tensile Strength: Yield (Proof), MPa 170 to 260
750

Thermal Properties

Latent Heat of Fusion, J/g 530
280
Maximum Temperature: Mechanical, °C 170
810
Melting Completion (Liquidus), °C 680
1450
Melting Onset (Solidus), °C 590
1410
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 110
16
Thermal Expansion, µm/m-K 21
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
13
Density, g/cm3 2.6
7.9
Embodied Carbon, kg CO2/kg material 7.8
2.9
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1070
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 13
150
Resilience: Unit (Modulus of Resilience), kJ/m3 190 to 470
1420
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 53
25
Strength to Weight: Axial, points 19 to 34
33
Strength to Weight: Bending, points 27 to 39
27
Thermal Diffusivity, mm2/s 48
4.4
Thermal Shock Resistance, points 8.5 to 15
33

Alloy Composition

Aluminum (Al), % 85.8 to 90.6
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
12 to 15
Copper (Cu), % 0 to 0.6
0 to 0.3
Iron (Fe), % 0 to 1.3
74 to 81.9
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.35
0.5 to 1.0
Molybdenum (Mo), % 0
1.5 to 2.0
Nickel (Ni), % 0 to 0.5
4.0 to 7.0
Nitrogen (N), % 0
0.060 to 0.12
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 9.0 to 10
0 to 0.5
Sulfur (S), % 0
0 to 0.0050
Tin (Sn), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.5
0
Residuals, % 0 to 0.25
0